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Facility requirements for helicopter noise researchDevelopment of future helicopter noise prediction methods requires an accurate experimental data base for correlation studies or assessment of theoretical prediction methods. The aerodynamic and acoustic performance criteria for conducting experimental studies of helicopter noise using existing test facilities were defined. Requirements for ground-based facilities were described in addition to the limitations associated with full scale and model scale studies. Flight testing methods were also evaluated briefly and the restrictions associated with these approaches were cited. Finally, a general evaluation of ground-based and flight testing methods is given. Based on this presentation, future investigators can select the experimental approach best suited for generating a desired data base. Also, facility improvements need to extend the state of the art in helicopter noise experimental studies so that problems can be identified.
Document ID
19840021603
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schlinker, R. H.
(United Technologies Research Center East Hartford, CT, United States)
Hoad, D. R.
(Army Structures Lab. Hampton, Va., United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1982
Publication Information
Publication: NASA. Langley Research Center Rotorcraft Noise
Subject Category
Acoustics
Accession Number
84N29672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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